EP1943369B1 - Method for coating a component - Google Patents

Method for coating a component Download PDF

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Publication number
EP1943369B1
EP1943369B1 EP06805414.7A EP06805414A EP1943369B1 EP 1943369 B1 EP1943369 B1 EP 1943369B1 EP 06805414 A EP06805414 A EP 06805414A EP 1943369 B1 EP1943369 B1 EP 1943369B1
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EP
European Patent Office
Prior art keywords
layer
coating
metallic
spraying
adhesive layer
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EP06805414.7A
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German (de)
French (fr)
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EP1943369A1 (en
Inventor
Thorsten Stoltenhoff
Klaus Gorris
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Praxair ST Technology Inc
Praxair Technology Inc
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Praxair ST Technology Inc
Praxair Technology Inc
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Publication of EP1943369A1 publication Critical patent/EP1943369A1/en
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Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/02Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/322Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer only coatings of metal elements only
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/324Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal matrix material layer comprising a mixture of at least two metals or metal phases or a metal-matrix material with hard embedded particles, e.g. WC-Me
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • C23C28/345Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
    • C23C28/3455Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • C23C28/347Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with layers adapted for cutting tools or wear applications
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/12Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying

Definitions

  • the invention relates to the production of functional surfaces on fiber-reinforced composite materials using thermal and kinetic spraying, wherein the protection of the component surface against wear, mechanical damage, deposits and adhesions, and the improvement in terms of sheet delivery (release behavior) is given a special significance.
  • Fiber reinforced composites can be used to manufacture components having exceptional mechanical and physical properties, e.g. have a low density, a high tensile and torsional strength, and a high elastic modulus or a high stiffness.
  • a variety of high strength fiber materials can be used, including carbon fibers, glass fibers, silicon carbide fibers, and many other oxides, carbides, and other materials.
  • a wide variety of polymeric materials including thermosetting resins, e.g. Phenolic resins, epoxy resins and many other materials.
  • the fibers can be very long and arranged in specific patterns, or they can be relatively short and random.
  • long fibers When arranged in specific patterns, long fibers may be oriented in a single direction or arranged in patterns designed to give the fiber reinforced composite a two- or three-dimensional strength.
  • the mechanical properties of the structure of the fiber reinforced composite material can be tailored to the specific requirements of a component.
  • the surfaces of fiber reinforced composites have low wear resistance, especially to adhesive, abrasive, and erosive wear, and their adhesion and wetting properties are inadequate for many applications, such as in the paper industry.
  • they are often susceptible to oxidation or other forms of corrosion, require heat protection, lack the necessary optical and electrical characteristics, and the like.
  • the insert is fiber reinforced Composite materials in many applications limits or requires the use of metallic or ceramic inserts or coatings in those areas that are exposed to contact with other components or fabrics and thus to increased wear.
  • the use of fiber reinforced composite rolls in the printing, paper and film industries is particularly interesting because they are much lighter and stiffer, and therefore easier and safer to handle than, for example, steel rolls, and thus less energy due to their lower inertia and time for their acceleration and deceleration, allowing for cost savings not only in handling and assembly but also in operation.
  • the rolls in this case have a metallic, ceramic or carbide coating or mixtures thereof with plastics, which provides the required wear resistance and other necessary properties.
  • thermal spray techniques a wide variety of metallic and ceramic layers, cermet layers, i. Carbide particles embedded in a metallic matrix, and some polymer coatings are produced.
  • the thermal spray family includes detonation spraying (including Super D-Gun TM ), high-velocity flame spraying and its variants such as air-fuel injection, plasma spraying, flame spraying and electric wire arc spraying.
  • detonation spraying including Super D-Gun TM
  • high-velocity flame spraying and its variants such as air-fuel injection, plasma spraying, flame spraying and electric wire arc spraying.
  • the sprayed material in the form of powder, wire, or rods is heated to a temperature that is at or slightly above its melting point, and droplets or fused particles of the material are accelerated in a gas stream.
  • the droplets are directed against the surface of the substrate to be coated (the portion or component) where they adhere, solidify and form a continuous layer of lamellar structure.
  • the discontinuous detonation spray process the layer of individual overlapping, firmly joined spray marks is formed.
  • Such methods are known in the art and described in detail in numerous publications.
  • a layer is first formed on the surface of a fiber reinforced composite material, which consists of a mixture of a synthetic resin and dispersed therein metallic particles. Upon curing of this layer, the surface is mechanically processed to expose the dispersed particles to chemically bond the particulate material to an outer layer material that is thermally sprayed onto the first layer.
  • a fiber reinforced composite material which consists of a mixture of a synthetic resin and dispersed therein metallic particles.
  • the surface is mechanically processed to expose the dispersed particles to chemically bond the particulate material to an outer layer material that is thermally sprayed onto the first layer.
  • a primer is applied to a plastic surface by means of a thermal spraying process, which may be in particular zinc, zinc alloys, aluminum alloys and / or exothermically reacting materials in the injection process, such as nickel-aluminum alloys. Subsequently, a functional coating likewise produced by means of a thermal spraying process is applied to the primer.
  • a thermal spraying process which may be in particular zinc, zinc alloys, aluminum alloys and / or exothermically reacting materials in the injection process, such as nickel-aluminum alloys.
  • EP 1 129 787 B1 describes a coating process in which a fiber reinforced composite body is coated with a first layer containing only polymer, a second layer of a polymer / metal mixture and then a thermal spray coating. To one To achieve sufficient bond strength between the layers, suitable polymer materials must be selected for the first two coating layers.
  • US 2002/187292 A1 describes a method for coating a component made of fiber-reinforced plastic, in which first a coating of hard rubber or thermoplastic with a metal or ceramic dispersion content of 5 vol% to 80 vol% is applied to the body of fiber-reinforced plastic, the applied coating is sanded until the dispersed metal or ceramic particles are to be seen on the surface, and then a functional layer of metal and / or ceramic is applied to the ground surface by means of thermal spraying.
  • the present invention is concerned in particular with the task of improving the wear resistance of fiber-reinforced plastics by combining two or more thermally or kinetically sprayed layer systems.
  • a thermally sprayed layer of a composite consisting of organic and metallic components is applied as an adhesive layer; on the adhesive layer, a thermally or kinetically sprayed layer with predominantly metallic portions is applied as an intermediate layer; and to the intermediate layer a thermally or kinetically sprayed functional metal cover layer, CERMET (metal-carbide composite), oxide ceramics or mixtures of the aforementioned materials, or mixtures thereof with plastic is applied.
  • CERMET metal-carbide composite
  • oxide ceramics or mixtures of the aforementioned materials, or mixtures thereof with plastic is applied.
  • the wire or powdered spray material itself may consist of the composite material.
  • the object of the so-called adhesive layer is to create a better connection to the matrix of the fiber-reinforced base material by the plastic content, and at the same time to ensure a better wetting of free Ilegender fibers, which also has a favorable effect on the layer adhesion.
  • the metallic components of the adhesive layer have the purpose of allowing a connection of the subsequently applied metallic intermediate layer.
  • This intermediate layer is essential for the final application of the functional topcoat. It serves as a stable substrate of the usually brittle, wear-resistant cover layer and at the same time brings about a moderate adaptation of the moduli of elasticity of the adhesive layer and cover layer.
  • the metallic intermediate layer ensures uniform distribution and removal of the introduced heat. Without sufficient heat dissipation, local evaporation of the organic binder of the main body may occur, which in turn would result in detachment of the entire layer system.
  • the method proposed here makes it possible to produce coated components from fiber-reinforced composite materials which are also suitable for strong dynamic loads and components with a large layer area.
  • the proportion of the organic matrix in the adhesion layer e.g. Polyester, between 5 and 60%, more preferably between 20 and 50%, and most preferably between 30 and 40%.
  • the metallic portion of the adhesive layer e.g. Aluminum, copper or nickel is preferably between 40 and 90%, more preferably between 60 and 80%.
  • the thickness of the adhesive layer is preferably 0.1 to 2 mm, more preferably 0.1 to 1 mm, and particularly preferably 0.2 to 0.4 mm.
  • a 0.2 mm thick adhesive layer is applied by plasma spraying and consists of a metal-polyester composite.
  • an approximately 0.1 to 1 mm thick metallic layer is sprayed onto the adhesive layer by a thermal spraying process.
  • the thickness of the intermediate layer is 0.5 to 2 mm.
  • the intermediate layer can be processed before the application of the cover layer, for example by grinding or turning to compensate for unevenness from previous operations.
  • the metallic intermediate layer is applied by means of a combustion-free method, such as arc spraying, plasma spraying or kinetic spraying In order to keep the heat input in the base material made of fiber-reinforced plastic as low as possible.
  • the intermediate layer already consists of a metal-hard material composite, e.g. a kinetically sprayed aluminum-aluminum oxide composite layer to achieve an increase in strength.
  • the functional top layer of the layer system is preferably an oxide ceramic (e.g., chromium oxide) or a CERMET (metal-carbide composite, e.g., tungsten carbide particles incorporated into a metallic cobalt matrix).
  • oxide ceramic e.g., chromium oxide
  • CERMET metal-carbide composite, e.g., tungsten carbide particles incorporated into a metallic cobalt matrix

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Metallurgy (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Organic Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Ceramic Engineering (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)

Description

Die Erfindung betrifft die Erzeugung funktioneller Oberflächen auf faserverstärkten Verbundmaterialien unter Anwendung des thermischen und kinetischen Spritzens, wobei dem Schutz der Bauteiloberfläche gegen Verschleiß, mechanische Beschädigungen, Belegen und Anhaftungen, sowie der Verbesserung hinsichtlich Blattabgabe (Releaseverhalten) eine besondere Bedeutung beigemessen wird.The invention relates to the production of functional surfaces on fiber-reinforced composite materials using thermal and kinetic spraying, wherein the protection of the component surface against wear, mechanical damage, deposits and adhesions, and the improvement in terms of sheet delivery (release behavior) is given a special significance.

Mit faserverstärkten Verbundmaterialien, insbesondere solchen mit einer Polymermatrix sowie kohlefaserverstärkten Polymeren, lassen sich Bauteile fertigen, die außerordentliche mechanische und physikalische Eigenschaften wie z.B. eine geringe Dichte, eine hohe Zug- und Torsionsfestigkeit, und einen hohen Elastizitätsmodul bzw. eine hohe Steifheit aufweisen. Eine Vielzahl von hochfesten Fasermaterialien können verwendet werden, einschließlich Kohlefasern, Glasfasern, Silizium-Carbid-Fasern und Fasern vieler weiterer Oxide, Carbide und anderer Materialien. Ebenso können eine große Vielzahl von Polymermaterialien einschließlich wärmehärtbarer Harze wie z.B. Phenolharze, Epoxidharze und vieler andere Materialien benutzt werden. Die Fasern können sehr lang sein und in spezifischen Mustern angeordnet werden, oder sie können relativ kurz und zufällig verteilt sein. Wenn lange Fasern in spezifischen Mustern angeordnet werden, können sie in einer einzigen Richtung ausgerichtet oder in Mustern angeordnet sein, die dazu ausgelegt sind, dem faserverstärkten Verbundwerkstoff eine zwei- oder dreidimensionale Festigkeit zu verleihen. Somit können die mechanischen Eigenschaften der Struktur des faserverstärkten Verbundwerkstoffes auf die spezifischen Erfordernisse einer Komponente abgestimmt werden.Fiber reinforced composites, particularly those having a polymer matrix and carbon fiber reinforced polymers, can be used to manufacture components having exceptional mechanical and physical properties, e.g. have a low density, a high tensile and torsional strength, and a high elastic modulus or a high stiffness. A variety of high strength fiber materials can be used, including carbon fibers, glass fibers, silicon carbide fibers, and many other oxides, carbides, and other materials. Likewise, a wide variety of polymeric materials, including thermosetting resins, e.g. Phenolic resins, epoxy resins and many other materials. The fibers can be very long and arranged in specific patterns, or they can be relatively short and random. When arranged in specific patterns, long fibers may be oriented in a single direction or arranged in patterns designed to give the fiber reinforced composite a two- or three-dimensional strength. Thus, the mechanical properties of the structure of the fiber reinforced composite material can be tailored to the specific requirements of a component.

Unglücklicherweise verfügen die Oberflächen faserverstärkter Verbundwerkstoffe über eine niedrige Verschleißbeständigkeit, insbesondere gegenüber Adhäsiv-, Abrasiv- und Erosiwerschleiß und ihre Haft- und Benetzungseigenschaften sind für viele Anwendungen wie etwa in der Papierindustrie unzureichend. Außerdem sind sie oftmals anfällig für Oxidation oder andere Formen der Korrosion, benötigen einen Wärmeschutz, verfügen nicht über die notwendigen optischen und elektrischen Charakteristika und dergleichen. Infolgedessen ist der Einsatz faserverstärkter Verbundwerkstoffe bei vielen Anwendungen begrenzt oder erfordert die Verwendung von metallischen oder keramischen Einsätzen oder Überzügen in denjenigen Bereichen, die einem Kontakt mit anderen Bauteilen oder Stoffen und damit einem erhöhten Verschleiß ausgesetzt sind.Unfortunately, the surfaces of fiber reinforced composites have low wear resistance, especially to adhesive, abrasive, and erosive wear, and their adhesion and wetting properties are inadequate for many applications, such as in the paper industry. In addition, they are often susceptible to oxidation or other forms of corrosion, require heat protection, lack the necessary optical and electrical characteristics, and the like. As a result, the insert is fiber reinforced Composite materials in many applications limits or requires the use of metallic or ceramic inserts or coatings in those areas that are exposed to contact with other components or fabrics and thus to increased wear.

Trotzdem ist der Einsatz von Walzen aus faserverstärkten Verbundwerkstoffen in der Druck-, Papier- und Folienindustrie besonders interessant, da sie wesentlich leichter und steifer und dadurch einfacher und sicherer zu handhaben sind als beispielsweise aus Stahl gefertigte Walzen, und so aufgrund ihrer geringeren Trägheit weniger Energie und Zeit für ihre Beschleunigung und Abbremsung erfordern, was nicht nur bei der Handhabung und Montage sondern auch im Betrieb Kosteneinsparungen ermöglicht. Um die Arbeitsflächen der Walzen mit den erforderlichen Eigenschaften zu versehen, weisen die Walzen hierbei einen metallischen, keramischen oder karbidischen Überzug oder Mischungen davon mit Kunststoffen auf, der den erforderlichen Verschleißwiderstand sowie andere notwendige Eigenschaften liefert. Unter Verwendung thermischer Spritzverfahren können eine große Vielzahl von metallischen und keramischen Schichten, Cermet-Schichten, d.h. Karbidpartikel eingelagert in eine metallische Matrix, sowie einige Polymerüberzüge hergestellt werden.Nevertheless, the use of fiber reinforced composite rolls in the printing, paper and film industries is particularly interesting because they are much lighter and stiffer, and therefore easier and safer to handle than, for example, steel rolls, and thus less energy due to their lower inertia and time for their acceleration and deceleration, allowing for cost savings not only in handling and assembly but also in operation. In order to provide the working surfaces of the rolls with the required properties, the rolls in this case have a metallic, ceramic or carbide coating or mixtures thereof with plastics, which provides the required wear resistance and other necessary properties. Using thermal spray techniques, a wide variety of metallic and ceramic layers, cermet layers, i. Carbide particles embedded in a metallic matrix, and some polymer coatings are produced.

Die Familie der thermischen Spritzverfahren beinhaltet das Detonationsspritzen (u.a. Super D-Gun), das Hochgeschwindigkeits-Flammspritzen und seine Varianten wie z.B. das Spritzen mit Luft-Brennstoff, das Plasmaspritzen, das Flammspritzen und das elektrische Drahtlichtbogen-Spritzen. In den meisten thermischen Beschichtungsverfahren wird der Spritzwerkstoff in Form von Pulver-, Draht-, oder Stangen auf eine Temperatur erhitzt, die bei oder etwas über seinem Schmelzpunkt liegt, und Tröpfchen oder angeschmolzene Partikel des Materials werden in einem Gasstrom beschleunigt. Die Tröpfchen werden gegen die Oberfläche des zu beschichtenden Substrats (des Abschnitts bzw. der Komponente) geleitet, wo sie anhaften, erstarren und eine zusammenhängende Schicht mit lamellenartiger Struktur bilden. Als Besonderheit des diskontinuierlich arbeitenden Detonationsspritzprozesses entsteht die Schicht aus einzelnen überlappenden, fest zusammengefügten Spritzflecken. Derartige Verfahren sind dem Fachmann bekannt und in zahlreichen Druckschriften ausführlich beschrieben.The thermal spray family includes detonation spraying (including Super D-Gun ), high-velocity flame spraying and its variants such as air-fuel injection, plasma spraying, flame spraying and electric wire arc spraying. In most thermal coating processes, the sprayed material in the form of powder, wire, or rods is heated to a temperature that is at or slightly above its melting point, and droplets or fused particles of the material are accelerated in a gas stream. The droplets are directed against the surface of the substrate to be coated (the portion or component) where they adhere, solidify and form a continuous layer of lamellar structure. As a special feature of the discontinuous detonation spray process, the layer of individual overlapping, firmly joined spray marks is formed. Such methods are known in the art and described in detail in numerous publications.

Obschon viele Versuche unternommen wurden, thermische Spritzschichten auf Metall-, Keramik- oder Karbidbasis direkt auf Oberflächen von faserverstärkten Verbundwerkstoffen aufzubringen, konnte üblicherweise nur eine geringe Schichthaftung erzielt werden, oftmals hafteten die Schichten nicht an dem faserverstärkten Untergrund an oder blätterten bereits nach Abscheidung einer kleinen Schichtdicke ab. Üblicherweise wird die Bauteiloberfläche vor dem Aufbringen der thermischen Spritzschicht zur Verbesserung der Haftung aufgeraut. Das Aufrauen erfolgt meist durch Korundstrahlen der Oberfläche. Korundstrahlen oder andere Formen des Aufrauens der zu beschichtenden Oberflächen kann jedoch zu einer nicht akzeptablen Erosion der Polymermatrix verbunden mit einer Freilegung der Fasern führen. Letzteres wiederum kann die Schichteigenschaften nachhaltig beeinträchtigen.While many attempts have been made to apply thermal, metal, ceramic or carbide based spray coatings directly to surfaces of fiber reinforced composites, usually only a low layer adhesion has been achieved, often the layers do not adhere to the fiber reinforced substrate or flake even after deposition of a small one layer thickness from. Typically, the component surface is roughened prior to application of the thermal spray coating to improve adhesion. The roughening is usually done by corundum blasting of the surface. However, corundum blasting or other forms of roughening of the surfaces to be coated may result in unacceptable erosion of the polymer matrix associated with exposure of the fibers. The latter, in turn, can permanently affect the layer properties.

Diese und weitere Probleme haben sich zum Beispiel bei der Anwendung des in US-A-5 857 950 beschriebenen Verfahrens ergeben. Hier wird die Oberfläche einer Kohlefaser-Walze sandgestrahlt und anschließend wird eine als Hitzeschild wirkende Zinkbeschichtung aufgebracht. Nach einem erneuten Sandstrahlen der nun zinkbeschichteten Walze wird eine Haftbeschichtung aufgebracht, bei der es sich um ein Gemisch aus Aluminiumbronze und Polyester handeln kann. Anschließend wird die Haftbeschichtung sandgestrahlt und ein Keramik-Spritzüberzug aufgebracht und graviert. Dieses Verfahren hat sich als nicht akzeptabel erwiesen.These and other problems have become apparent, for example, in the application of in US-A-5,857,950 described method. Here, the surface of a carbon fiber roller is sandblasted and then applied as a heat shield zinc coating is applied. After re-sandblasting the now zinc-coated roller, an adhesive coating is applied, which may be a mixture of aluminum bronze and polyester. Subsequently, the adhesive coating is sandblasted and a ceramic sprayed coating applied and engraved. This procedure has proved unacceptable.

Ein alternatives Verfahren ist in EP 0 514 640 B1 dargestellt. Hierbei wird zuerst auf der Oberfläche eines faserverstärkten Verbundwerkstoffes eine Lage erzeugt, die aus einem Gemisch eines synthetischen Harzes und darin dispergierter metallischer Partikel besteht. Nach Aushärtung dieser Lage wird die Oberfläche mechanisch bearbeitet, um die dispergierten Partikel freizulegen, damit sich das Partikelmaterial mit einem äußeren Schichtwerkstoff, der auf die erste Lage thermisch aufgespritzt wird, chemisch verbinden kann. Obgleich sich mit diesem Verfahren begrenzte Erfolge erzielen ließen, kann das Gemisch aus synthetischem Harz und Partikelmaterial an dem Verbundwerkstoff nicht gut anhaften und neigt dazu, Materialkügelchen auf der Oberfläche auszubilden, wodurch es für eine kommerzielle Herstellung ungeeignet ist.An alternative method is in EP 0 514 640 B1 shown. Here, a layer is first formed on the surface of a fiber reinforced composite material, which consists of a mixture of a synthetic resin and dispersed therein metallic particles. Upon curing of this layer, the surface is mechanically processed to expose the dispersed particles to chemically bond the particulate material to an outer layer material that is thermally sprayed onto the first layer. Although limited success has been achieved with this method, the mixture of synthetic resin and particulate material can not adhere well to the composite and tends to form globules of material on the surface, rendering it unsuitable for commercial production.

In der DE 100 37 212 A1 wird auf einer Kunststoffoberfläche mittels eines thermischen Spritzverfahrens ein Haftgrund aufgebracht, bei dem es sich insbesondere um Zink, Zinklegierungen, Aluminiumlegierungen und/oder im Spritzprozess exotherm reagierende Materialien wie Nickel-Aluminium-Legierungen handeln kann. Anschließend wird auf dem Haftgrund eine ebenfalls mittels eines thermischen Spritzverfahrens erzeugte Funktionsbeschichtung aufgebracht.In the DE 100 37 212 A1 For example, a primer is applied to a plastic surface by means of a thermal spraying process, which may be in particular zinc, zinc alloys, aluminum alloys and / or exothermically reacting materials in the injection process, such as nickel-aluminum alloys. Subsequently, a functional coating likewise produced by means of a thermal spraying process is applied to the primer.

Des Weiteren ist in der EP 1 129 787 B1 ein Beschichtungsverfahren beschrieben, bei welchem ein Grundkörper aus faserverstärktem Verbundwerkstoff mit einer ersten Lage, die nur Polymer enthält, einer zweiten Lage aus einem Polymer/Metall-Gemisch und anschließend einem thermischem Spritzüberzug beschichtet wird. Um eine ausreichende Bindungsstärke zwischen den Schichten zu erreichen, müssen für die ersten beiden Beschichtungslagen geeignete Polymerwerkstoffe gewählt werden.Furthermore, in the EP 1 129 787 B1 describes a coating process in which a fiber reinforced composite body is coated with a first layer containing only polymer, a second layer of a polymer / metal mixture and then a thermal spray coating. To one To achieve sufficient bond strength between the layers, suitable polymer materials must be selected for the first two coating layers.

Ferner ist in US 2002/187292 A1 ein Verfahren zur Beschichtung eines Bauteils aus faserverstärktem Kunststoff beschrieben, bei welchem zuerst eine Beschichtung aus Hartgummi oder Thermoplast mit einem Metall- oder Keramikdispersionsanteil von 5 Vol % bis 80 Vol % auf den Grundkörper aus faservertärktem Kunststoff aufgebracht wird, die aufgebrachte Beschichtung angeschliffen wird, bis die eindispergierten Metall- oder Keramikpartikel an der Oberfläche zusehen sind, und anschließend auf die angeschliffene Oberfläche eine Funktionsschicht aus Metall und/oder Keramik mittels thermischem Spritzen aufgebracht wird.Furthermore, in US 2002/187292 A1 describes a method for coating a component made of fiber-reinforced plastic, in which first a coating of hard rubber or thermoplastic with a metal or ceramic dispersion content of 5 vol% to 80 vol% is applied to the body of fiber-reinforced plastic, the applied coating is sanded until the dispersed metal or ceramic particles are to be seen on the surface, and then a functional layer of metal and / or ceramic is applied to the ground surface by means of thermal spraying.

Der vorliegenden Erfindung liegt die Aufgabe zugrunde, beschichtete faserverstärkte Verbundpolymermaterialien bereitzustellen, bei welchen die Haftung der Beschichtungslagen an dem Verbundwerkstoff noch weiter verbessert ist. Die vorliegende Erfindung befasst sich dabei insbesondere mit der Aufgabenstellung, durch Kombination zweier oder mehrerer thermisch oder kinetisch gespritzter Schichtsysteme die Verschleißbeständigkeit von faserverstärkten Kunststoffen zu verbessern.It is an object of the present invention to provide coated fiber reinforced composite polymer materials in which the adhesion of the coating layers to the composite is even further improved. The present invention is concerned in particular with the task of improving the wear resistance of fiber-reinforced plastics by combining two or more thermally or kinetically sprayed layer systems.

Diese Aufgabe wird erfindungsgemäß dadurch gelöst, dass auf die Oberfläche des faserverstärkten Kunststoffs zunächst eine thermisch gespritzte Schicht aus einem Verbund bestehend aus organischen und metallischen Anteilen als Haftschicht aufgebracht wird; auf die Haftschicht eine thermisch oder kinetisch gespritzte Schicht mit überwiegend metallischen Anteilen als Zwischenschicht aufgebracht wird; und auf die Zwischenschicht eine thermisch oder kinetisch gespritzte funktionelle Deckschicht aus Metall, CERMET (Metall-Karbid-Verbund), Oxidkeramik oder Mischungen aus den vorgenannten Materialien, oder Mischungen davon mit Kunststoff aufgebracht wird. Für den als Haftschicht aufgebrachten Metall-KunststoffVerbund kann hierbei während des Spritzens ein Gemisch aus zwei oder mehreren unterschiedlichen Werkstoffen verwendet werden. Anstatt während des Spritzens zwei oder mehr Tellströme zu verwenden, kann das draht- oder pulverförmige Spritzmaterial selbst aus dem Werkstoffverbund bestehen.This object is achieved in that on the surface of the fiber-reinforced plastic, first a thermally sprayed layer of a composite consisting of organic and metallic components is applied as an adhesive layer; on the adhesive layer, a thermally or kinetically sprayed layer with predominantly metallic portions is applied as an intermediate layer; and to the intermediate layer a thermally or kinetically sprayed functional metal cover layer, CERMET (metal-carbide composite), oxide ceramics or mixtures of the aforementioned materials, or mixtures thereof with plastic is applied. For the metal-plastic composite applied as an adhesive layer, a mixture of two or more different materials can be used during spraying. Instead of using two or more Tell streams during spraying, the wire or powdered spray material itself may consist of the composite material.

Aufgabe der so genannten Haftschicht ist es, durch den Kunststoffanteil eine bessere Anbindung an die Matrix des faserverstärkten Grundwerkstoffs zu schaffen, und gleichzeitig eine bessere Benetzung frei Ilegender Fasern sicherzustellen, welche sich ebenfalls günstig auf die Schichthaftung auswirkt. Die metallischen Anteile der Haftschicht haben den Zweck, eine Anbindung der nachfolgend aufzubringenden metallischen Zwischenschicht, zu ermöglichen.The object of the so-called adhesive layer is to create a better connection to the matrix of the fiber-reinforced base material by the plastic content, and at the same time to ensure a better wetting of free Ilegender fibers, which also has a favorable effect on the layer adhesion. The metallic components of the adhesive layer have the purpose of allowing a connection of the subsequently applied metallic intermediate layer.

Diese Zwischenschicht ist für das abschließende Aufbringen der funktionellen Deckschicht essentiell. Sie dient als stabiler Untergrund der zumeist spröden, verschleißbeständigen Deckschicht und bewirkt gleichzeitig eine moderate Anpassung der E-Moduli von Haftschicht und Deckschicht. Außerdem sorgt die metallische Zwischenschicht bei der weiteren Beschichtung des Bauteils etwa durch Hochgeschwindigkeits-Flammspritzen oder durch Detonationsspritzen für eine gleichmäßige Verteilung und Abfuhr der eingebrachten Wärme. Ohne ausreichende Wärmeabfuhr kann es zu einem örtlich auftretenden Verdampfen des organischen Binders des Grundkörpers kommen, was wiederum eine Ablösung des gesamten Schichtsystems zur Folge hätte.This intermediate layer is essential for the final application of the functional topcoat. It serves as a stable substrate of the usually brittle, wear-resistant cover layer and at the same time brings about a moderate adaptation of the moduli of elasticity of the adhesive layer and cover layer. In addition, in the further coating of the component, for example by high-speed flame spraying or by detonation spraying, the metallic intermediate layer ensures uniform distribution and removal of the introduced heat. Without sufficient heat dissipation, local evaporation of the organic binder of the main body may occur, which in turn would result in detachment of the entire layer system.

Mit dem hier vorgeschlagenen Verfahren lassen sich beschichtete Bauteile aus faserverstärkten Verbundwerkstoffen herstellen, die sich auch für starke dynamische Beanspruchungen eignen sowie Bauteile mit großer Schichtfläche.The method proposed here makes it possible to produce coated components from fiber-reinforced composite materials which are also suitable for strong dynamic loads and components with a large layer area.

Bevorzugte Ausgestaltungen der Erfindung ergeben sich aus den Unteransprüchen.Preferred embodiments of the invention will become apparent from the dependent claims.

Vorzugsweise liegt der Anteil der organischen Matrix in der Haftschicht, z.B. Polyester, zwischen 5 und 60 %, stärker bevorzugt zwischen 20 und 50 %, und besonders bevorzugt zwischen 30 und 40 %.Preferably, the proportion of the organic matrix in the adhesion layer, e.g. Polyester, between 5 and 60%, more preferably between 20 and 50%, and most preferably between 30 and 40%.

Der metallische Anteil der Haftschicht, z.B. Aluminium, Kupfer oder Nickel, liegt vorzugsweise zwischen 40 und 90 %, stärker bevorzugt zwischen 60 und 80 %.The metallic portion of the adhesive layer, e.g. Aluminum, copper or nickel is preferably between 40 and 90%, more preferably between 60 and 80%.

Die Dicke der Haftschicht beträgt vorzugsweise 0,1 bis 2 mm, stärker bevorzugt 0,1 bis 1 mm, und besonders bevorzugt 0,2 bis 0,4 mm.The thickness of the adhesive layer is preferably 0.1 to 2 mm, more preferably 0.1 to 1 mm, and particularly preferably 0.2 to 0.4 mm.

In einer besonders bevorzugten Ausführungsform wird eine 0,2 mm dicke Haftschicht durch Plasmaspritzen aufgebracht und besteht aus einem Metall-Polyester-Verbund. In einer anderen bevorzugten Ausführungsform wird auf die Haftschicht durch ein thermisches Spritzverfahren eine etwa 0,1 bis 1 mm dicke metallische Schicht aufgespritzt.In a particularly preferred embodiment, a 0.2 mm thick adhesive layer is applied by plasma spraying and consists of a metal-polyester composite. In another preferred embodiment, an approximately 0.1 to 1 mm thick metallic layer is sprayed onto the adhesive layer by a thermal spraying process.

In einer Ausführung beträgt die Dicke der Zwischenschicht 0,5 bis 2 mm. Die Zwischenschicht kann vor dem Aufbringen der Deckschicht beispielsweise durch Schleifen oder Drehen bearbeitet werden, um Unebenheiten aus vorhergehenden Arbeitsschritten auszugleichen.In one embodiment, the thickness of the intermediate layer is 0.5 to 2 mm. The intermediate layer can be processed before the application of the cover layer, for example by grinding or turning to compensate for unevenness from previous operations.

Günstig ist, wenn die metallische Zwischenschicht durch ein verbrennungsfreies Verfahren etwa Lichtbogenspritzen, Plasmaspritzen oder kinetisches Spritzen aufgebracht wird, um den Wärmeeintrag in den Grundwerkstoff aus faserverstärktem Kunststoff so gering wie möglich zu halten.It is favorable if the metallic intermediate layer is applied by means of a combustion-free method, such as arc spraying, plasma spraying or kinetic spraying In order to keep the heat input in the base material made of fiber-reinforced plastic as low as possible.

Günstig ist auch, wenn für die Zwischenschicht ein metallischer Werkstoff mit möglichst hoher Duktilität verwendet wird.It is also favorable if a metallic material with the highest possible ductility is used for the intermediate layer.

In einer weiteren Ausführung besteht bereits die Zwischenschicht aus einem Metall-Hartstoff-Verbund, z.B. eine kinetisch gespritzte Aluminium-Aluminiumoxid-Verbundschicht, um eine Erhöhung der Festigkeit zu erreichen.In a further embodiment, the intermediate layer already consists of a metal-hard material composite, e.g. a kinetically sprayed aluminum-aluminum oxide composite layer to achieve an increase in strength.

Wenn die Beschichtung des faserverstärkten Werkstoffs insbesondere eine Erhöhung der Verschleißbeständigkeit zum Ziel hat, besteht die funktionelle Deckschicht des Schichtsystems vorzugsweise aus einer Oxidkeramik (z.B. Chromoxid) oder einem CERMET (Metall-Karbid-Verbund, z.B. Wolframkarbidpartikel eingelagert In eine metallische Kobaltmatrix).In particular, if the coating of the fiber-reinforced material is intended to increase wear resistance, the functional top layer of the layer system is preferably an oxide ceramic (e.g., chromium oxide) or a CERMET (metal-carbide composite, e.g., tungsten carbide particles incorporated into a metallic cobalt matrix).

Claims (7)

  1. Method for coating a member of fiber-reinforced composite material, characterized in that
    (a) at first a composite consisting of organic and metallic components is applied by means of thermal spraying as an adhesive layer to a surface of the member to be coated;
    (b) a layer predominantly comprising metallic components is applied by means of thermal or kinetic spraying as an intermediate layer to said adhesive layer; and
    (c) a functional covering layer consisting of metal, a metal-carbide composite, oxide ceramics or mixtures of said materials is applied to said intermediate layer by means of thermal or kinetic spraying.
  2. Method as claimed in claim 1, characterized in that the organic component of the adhesive layer amounts to between 5 and 60 %, preferably between 20 and 50 %, and most preferably between 30 and 40 %.
  3. Method as claimed in claim 1, characterized in that the metallic component of the adhesive layer amounts to between 40 and 90 %, and preferably between 60 and 80 %.
  4. Method as claimed in any one of the preceding claims, characterized in that the thickness of the adhesive layer is between 0.1 and 2 mm, preferably between 0.1 and 1 mm, and more preferably between 0.2 and 0.4 mm.
  5. Method as claimed in any one of the preceding claims, characterized in that the metallic component of the intermediate layer amounts to 60 % or more.
  6. Method as claimed in any one of the preceding claims, characterized in that the thickness of the intermediate layer is between 0.1 and 2 mm, preferably between 0.2 and 1 mm, and most preferably between 0.3 and 0.6 mm.
  7. Method as claimed in any one of the preceding claims, characterized in that the intermediate layer is machined before applying the covering layer.
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